# Service difficulty reports: N928FD

A list on [N928FD](https://openairdocs.org/aircraft/N928FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 102 reports

- [SDR FDEA202608211220](https://openairdocs.org/sdr/FDEA202608211220.md): Oxygen Mask · no test · Aug 21, 2026 · N928FD · Boeing 75728A · Crew Oxygen System
  > DURING MX PREFLIGHT; CAPTAINS O2 MASK FAILS "PRESS TO TEST." REPLACED CAPT'S FULL FACE O2 MASK IAW B757 AMM CH. REF. LISTED ABOVE. OPS AND LEAK CKS GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202608211213](https://openairdocs.org/sdr/FDEA202608211213.md): Oxygen Mask · no test · Aug 21, 2026 · N928FD · Boeing 75728A · Crew Oxygen System
  > DURING MX PREFLIGHT, CAPTAINS O2 MASK FAILED A PRESS TO TEST. PREMATURE REMOVAL/INSTALLATION. REPLACED CAPT'S FULL FACE O2 MASK IAW AMM 35-11-51-4-99. OPS & LEAK CHKD GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202604020391](https://openairdocs.org/sdr/FDEA202604020391.md): Battery Pack · inoperative · Apr 2, 2026 · N928FD · Boeing 75728A · Emergency Lighting
  > ON PREFLIGHT FOUND R1 DOOR SLIDE LIGHT INOPERATIVE. AMM 33-51-06-2-1, AMM 33-51-07-2, & AMM 33-51-07-862-036. REPLACED BULB IN R1 DOOR SLIDE LIGHT IAW MM 33-51-06-2-1. REPLACED R1 DOOR SLIDE LIGHT POWER SUPPLY IN FWD GALLEY AND BATTERY PACK IAW MM 33-51-07
- [SDR FDEA202511112157](https://openairdocs.org/sdr/FDEA202511112157.md): Girt Bar · damaged · Nov 11, 2025 · N928FD · Boeing 75728A · Passenger/Crew Doors
  > L1 DOOR WILL NOT OPEN. TROUBLESHOT L1 DOOR AND DISCOVERED FWD END OF GIRT BAR JAMMED IN ARMING SLIDER. REMOVED AND REPLACED L1 DOOR GIRT BAR REMOVED IAW AMM 25-66-10-2 AND PERFORMED L1 DOOR ADJUSTMENT TESTS PER AMM 52-11-25-5. L1 DOOR OPS AND FUNCTIONS NORMA
- [SDR FDEA202503110363](https://openairdocs.org/sdr/FDEA202503110363.md): Floor Panel · damaged · Mar 11, 2025 · N928FD · Boeing 75728A · Fuselage Floor Panel
  > FLOOR PANEL #252MWF HAS DAMAGE AND MISSING INSERTS, R/H AFT O/B MAIN CABIN FLOOR PANEL. FABRICATED FLOOR PANEL #252MWF ON VTMAE TRAVELER #T25/1800902 IAW STMAE DWG. #11864182 REV. D, MAJOR REPAIR.
- [SDR FDEA202503110362](https://openairdocs.org/sdr/FDEA202503110362.md): Floor Panel · damaged · Mar 11, 2025 · N928FD · Boeing 75728A · Fuselage Floor Panel
  > FLOOR PANEL #251MXF AFT MAIN CABIN L/H O/B HAS DAMAGE/MISSING INSERTS. FABRICATED FLOOR PANEL #251MXF ON VTMAE TRAVELER #T25/1800901 IAW STMAE DWG. #11864182 REV. D, MAJOR REPAIR.
- [SDR FDEA202502280308](https://openairdocs.org/sdr/FDEA202502280308.md): Seat Track · damaged · Feb 28, 2025 · N928FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT FS 980 BL 0 HAS DAMAGE. REMOVED AND REPLACED SEAT TRACK BETWEEN STA 879 TO 1065 BL 0 IAW SRM 51-40-02 FROM MATERIAL BAC 1520-2473 BATCH # 0002425804 IAW SRM 53-40-52-01 FIGURE 1 DETAIL II, MAJOR REPAIR.
- [SDR FDEA202501100051](https://openairdocs.org/sdr/FDEA202501100051.md): Gust Lock · failed · Jan 10, 2025 · N928FD · Boeing 75728A · Service Doors
  > R1 DOOR GUST LOCK INOP. R&R BROKEN GUST LOCK ON R1 DOOR. OPS CHK GOOD. OK FOR SVC.
- [SDR FDEA202501080038](https://openairdocs.org/sdr/FDEA202501080038.md): Flap System · malfunctioned · Jan 8, 2025 · N928FD · Boeing 75728A · Leading Edge Slat Control System
  > TE FLAP DISAGREE, EMERGENCY DECLARED. ON INITIAL TROUBLESHOOTING NO EICAS MSG NOTED FOR TE FLAP DISAGREE. PUT FLAPS BACK TO NORMAL CONFIG FROM ALT MODE. BITE CHECKED ALL 3 FSEU S AND NO FAULTS NOTED. FLAP SELECTOR LEVER CLEANED AND LUBED AS PRECAUTION.
- [SDR FDEA202409231342](https://openairdocs.org/sdr/FDEA202409231342.md): Bottle · low pressure · Sep 23, 2024 · N928FD · Boeing 75728A · Emergency Equipment
  > ON SERVICE CHECK FOUND R1 DOOR EMERGENCY RESEVOIR BELOW MINIMUM REQUIRED PRESSURE. AMM: 52-11-30-4 REMOVED AND REPLACED RI DOOR ASSIST BOTTLE PER ABOVE B757 REF.
- [SDR FDEA202405310754](https://openairdocs.org/sdr/FDEA202405310754.md): Ferrule · damaged · May 31, 2024 · N928FD · Boeing 75728A · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. AMM: 33-51-06-2-1 RELAMPED, NO HELP. FOUND LIGHT WOULD INTERMITTENTLY COME ON WHEN MANIPULATING LIGHT ASSY. REMOVED BULB AND FOUND LAMP BASE WORN AND PITTED. NEEDS NEW BASE, LIGHT ASSY IS REMOVED AND IN MX
- [SDR FDEA202401250111](https://openairdocs.org/sdr/FDEA202401250111.md): Engine · inoperative · Jan 25, 2024 · N928FD · Boeing 75728A · Engine (Turbine/Turboprop)
  > PDIS 928 73-22 1096 25JAN24 MEM OPEN U AT CRUISE, FL360, #1 ENG EPR DID NOT INDICATE PROPERLY. THE WHITE EPR NEEDLE WAS FULL POWER ABOVE THE DIAL, THE POWER STRIP WAS ALSO WELL ABOVE THE MAX PORTION, THE N1 WAS SLOWLY DEGRADING AND WE BEGAN T
- [SDR FDEA202212012864](https://openairdocs.org/sdr/FDEA202212012864.md): Control Panel · failed · Dec 1, 2022 · N928FD · Boeing 75728A · Emergency Lighting
  > OVERHEAD COCKPIT EMERGENCY LIGHTS PANEL WON'T TEST IAW AMM 33-51-08-4. REMOVED AND REPLACED P5 EMEGENCY LIGHTS PANEL IAW AMM 33-51-08-4. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA202110162545](https://openairdocs.org/sdr/FDEA202110162545.md): Warning Message · false activation · Oct 16, 2021 · N928FD · Boeing 75728A · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP DISAGREE. HANDLE AT 20. INDICATOR SAID BOTH FLAPS AT 15. RAN QRH. RECONFIGURED FLAPS FROM ALT TO REGULAR AND RAISED FLAPS. OPERATED FLAPS THROUGH ALL DETENTS FOR SEVERAL CYCLES, REF MM 27-51-00-5. NO FAULTS NOTED. PERFORMED BITE CK OF ALL
- [SDR FDEA202105231364](https://openairdocs.org/sdr/FDEA202105231364.md): Fairing · cracked · May 23, 2021 · N928FD · Boeing 75728A · Nacelle/Pylon Miscellaneous Structure
  > #2 ENG PYLON O/B LOWER FLEXABLE FAIRING CLOSEOUT PANEL IS CRACKED ABOVE EXHAUST NOZZLE REMOVED AND REPLACED PANEL PER DWG # 311N5137
- [SDR FDEA202105201323](https://openairdocs.org/sdr/FDEA202105201323.md): Stop Fitting · cracked · May 20, 2021 · N928FD · Boeing 75728A · Service Doors
  > R2 DOOR, 3RD FROM BOTTOM DOOR STOP IS CRACKED REMOVED AND REPLACED R-2 DOOR PER FEDEX B757 AMM 52-11-01-4
- [SDR FDEA202105181289](https://openairdocs.org/sdr/FDEA202105181289.md): Web · dented · May 18, 2021 · N928FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MCD AFT PRESSURE RELIEF DOOR INTERNAL CLOSE OUT WEB HAS SEVERAL INTERNALLY PROTRUDING DENTS AT THE UPPER EDGE OF THE WEB BETWEEN WL 210 AND 220, BETWEEN STA 580 AND 600 REMOVED, FABRICATED AND REPLACED WEB AS REQUIRED IAW BOEING DWG 65-49309 REV "D" AND B7
- [SDR FDEA202105181288](https://openairdocs.org/sdr/FDEA202105181288.md): Web · dented · May 18, 2021 · N928FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > MCD FWD PRESSURE RELIEF DOOR INTERNAL CLOSE OUT WEB HAS SEVERAL INTERNALLY PROTRUDING DENTS AT THE UPPER EDGE OF THE WEB BETWEEN WL 210 AND 220, BETWEEN STA 500 AND 520. REMOVED, FABRICATED AND REPLACED WEB AS REQ IAW BOEING DWG 65-49309 REV "D" AND B757 S
- [SDR FDEA202105121204](https://openairdocs.org/sdr/FDEA202105121204.md): Attach Angle · cracked · May 12, 2021 · N928FD · Boeing 75728A · Fuselage Main, Attach Fittings
  > LMLG WHEEL WELL FWD EDGE WING TO BODY PANEL ATTACH CLIP IS CRACKED 32" OUTBOARD OF KEEL BEAM. REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP PER BAC DWG 149N7550
- [SDR FDEA2020043090838](https://openairdocs.org/sdr/FDEA2020043090838.md): Fire Warning · false activation · Apr 29, 2020 · N928FD · Boeing 75728A · Fire Detection
  > UPON DESCENT INTO DESTINATION APPROXMATELY FL 180 IN IMC/RAIN RT ENG FIRE WARNING AND LIGHT CAME ON. RAN PHASE ONES AND QRH FOR RT ENG FIRE. UPON RT ENGINE SHUTDOWN, FIRE LIGHT WENT OUT THEN CAME BACK ON SO FOLLOWED QRH AND FIRED THE FIRE BOTTLE. RED LIGH
- [SDR FDEA201909272357](https://openairdocs.org/sdr/FDEA201909272357.md): Lanyard · out of position · Sep 27, 2019 · N928FD · Boeing 75728A · Emergency Equipment
  > RT CABIN ENTRY DOOR WILL NOT ARM FOUND LANYARD CORD STUCK IN GIRT BAR, PROPERLY STOWED LANYARD CORD. DOOR ARM LIGHT OPS CHECKED NORMAL PER AMM 52-71-00-5
- [SDR FDEA2019042290862](https://openairdocs.org/sdr/FDEA2019042290862.md): Bracket · corroded · Apr 19, 2019 · N928FD · Boeing 75728A · Fuselage Main, Structure
  > BS 1410, AFT CARGO DOOR, LOWER FRAME SUPPORT BRACKET HAS EXFOILIATING CORROSION, 1 INCH BY 1 INCH SIZE. BOTH SIDES OF BRACKET ARE CORRODED.
- [SDR FDEA201904160811](https://openairdocs.org/sdr/FDEA201904160811.md): Crease Beam · corroded · Apr 16, 2019 · N928FD · Boeing 75728A · Fuselage Main, Structure
  > MAIN CABIN CREASE BEAM STA. 860-880 RBL64.20 HAS CORROSION REMOVED CORR. ON CREASE BEAM STA 860-880 RBL 64.20 IAW B757 SRM 51-10-02. ORIG MAT.071 REM.051 LOSS.020 FOUND OUT OF LLIMITS IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. REMOVED, FABRICATED AND
- [SDR FDEA201904160810](https://openairdocs.org/sdr/FDEA201904160810.md): Seat Track · corroded · Apr 16, 2019 · N928FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE MAIN CABIN STA. 1540 RBL 45.50 PERFORMED SEAT TRACK REPAIR AT RBL 45.50 BETWEEN BS 1500-1540 IAW B757 SRM 53-00-52- 2R FIG 201 REPAIR 1 OPTION1. REMOVED COR ON SEAT TRACK IAW B757 SRM 51-10-02. 100% MAT. LOSS DUE TO EXFOILATION F
- [SDR FDEA201804241109](https://openairdocs.org/sdr/FDEA201804241109.md): Tube · damaged · Apr 24, 2018 · N928FD · Boeing 75728A · Engine Pressure Ratio (EPR)
  > PDIS 928 76-00 6718 24APR18 BNA OPEN U LOGPAGES:2252904 AT CRUISE NOTICED L EPR PEGGED. FUEL FLOW AT 1.5. LOTS OF RIGHT RUDDER. A/S STARTED TO DECREASE. NO EICAS. L ENG DID NOT RESPOND TO THROTTLE MOVEMENT. PART 24APR18 11:37 MC1 U IDENTIFIED PARTS COLD CU
- [SDR FDEA2018042601109](https://openairdocs.org/sdr/FDEA2018042601109.md): Tube · damaged · Apr 24, 2018 · N928FD · Boeing 75728A · Power Lever
  > DURING CRUISE, NOTICED THE LT EPR PEGGED. FUEL FLOW AT 1.5. A LOT OF RIGHT RUDDER. A/S STARTED TO DECREASE. NO EICAS. LT ENG DID NOT RESPOND TO THROTTLE MOVEMENT. FOUND THE P1 TUBE JUST AFT OF PROBE DAMAGED.
- [SDR FDEA201804090955](https://openairdocs.org/sdr/FDEA201804090955.md): Seat Track · gouged · Apr 9, 2018 · N928FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45.5, BS 580 CROWN AREA DAMAGED. INSTALLED A NEW SECTION OF SEAT TRACK IAW DWG 143N5090, REV-, SRM 51-40-05-0G, SRM 51-40-02-0G, SRM 51-20-01-0G, AMM 51-21-00-7, AND DWG 143N8750 REV-.
- [SDR FDEA201804090954](https://openairdocs.org/sdr/FDEA201804090954.md): Floorbeam · cracked · Apr 9, 2018 · N928FD · Boeing 75728A · Fuselage Main, Floor Beam
  > MAIN CABIN STA 580 FLOORBEAM STUB FITTING HAS A CRACK ON AFT FLANGE AT LBL 45. COMPLIED WITH EA F-5310-T0339360 P1.
- [SDR FDEA201802010285](https://openairdocs.org/sdr/FDEA201802010285.md): Tube · leaking · Feb 1, 2018 · N928FD · Boeing 75728A · Engine Pressure Ratio (EPR)
  > DURING CLIMB THROUGH FL 270, THE LEFT ENGINE INDICATED N1 OF 82% VS N1 95%, FOR THE RIGHT ENGINE. LEFT EGT WAS 120DEG. LOWER, N2 WAS 10% LOWER. RUDDER TRIM OF 4 RIGHT REQUIRED. LEVEL AT 270 ALL INDICATIONS THE SAME FOR BOTH ENGINES EPR 1.37, N1 75%, EG
- [SDR FDEA201707292081](https://openairdocs.org/sdr/FDEA201707292081.md): Engine · flamed out · Jul 29, 2017 · N928FD · Boeing 75728A · Engine (Turbine/Turboprop)
  > RT ENGINE FLAMED OUT ON ARRIVAL AT 15000 FT. AT BLOCK IN, THE RT ENG LP PUMP STATUS MESSAGE INDICATED. REMOVED AND REPLACED THE HIGH PRESSURE FUEL PUMP, ENGINE TRANSIENT PRESSURE UNIT, AND LOW PRESSURE FUEL PUMP IAW AMM 73-11-03-4-4, 73-11-01-4, AND 75-32-1
- [SDR FDEA201706161686](https://openairdocs.org/sdr/FDEA201706161686.md): Governor · malfunctioned · Jun 16, 2017 · N928FD · Boeing 75728A · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FAILED AT APPROXIMATELY 7000' MSL DURING DESCENT. INITIALLY NOTED RIGHT GENERATOR OFF, THEN UTILITY BUSSES, AUTOTHROTTLES, AND AUTOPILOT. ENGINE WAS A SLOW SHUTDOWN. RIGHT OIL PRESSURE WAS ZERO. WINDMILLED RIGHT ENGINE FOR 7 - 8 MINUTES. NO VIBR
- [SDR FDEA201704211249](https://openairdocs.org/sdr/FDEA201704211249.md): Terminal · loose · Apr 21, 2017 · N928FD · Boeing 75728A · Light System Wiring
  > EMERGENCY LIGHTS FAIL TO TEST WITH SWITCH ABOVE L1 DOOR IN COURIER COMPT. FOUND TERMINAL END OF WIRE W3532-0036-20 LOOSE AT GROUND STUD GD1420-DC. TIGHTENED TERMINAL STUD AND VERIFIED GROUND AT SWITCH S10292. REF WDM 33-51-12 AND SWPM. A/C REQUIRES REINSTALLAT
- [SDR FDEA201704111132](https://openairdocs.org/sdr/FDEA201704111132.md): Skin · damaged · Apr 11, 2017 · N928FD · Boeing 75728A · Trailing Edge Flaps
  > DURING REMOVAL OF INBOARD MAIN FLAP OUTBOARD FLAP FAIRING FWD INBOARD ATTACH BRACKET. FOUND THE SKIN MOUNT BOLT HOLES WORN AND ELONGATED. COMPLIED WITH EA 5750-TO332573 P1.
- [SDR FDEA201704061099](https://openairdocs.org/sdr/FDEA201704061099.md): Brace · cracked · Apr 6, 2017 · N928FD · Boeing 75728A · Nacelle/Pylon Miscellaneous Structure
  > TWO CRACK INDICATIONS AT THE INSIDE HOLES ON AFT SIDE OF NR 1 PYLON DIAGONAL BRACE FITTING LOWER SURFACE IN ALUMINUM ONLY. COMPLIED WITH EA F-5450-T0332370 B P1.
- [SDR FDEA201703301014](https://openairdocs.org/sdr/FDEA201703301014.md): Fitting · cracked · Mar 30, 2017 · N928FD · Boeing 75728A · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM BS 580, STUB BEAM FITTING AT LBL 44.5 HAS A CRACK IN UPPER RADIUS OF TOP FLANGE. REMOVED AND REPLACED THE STUB BEAM FITTING IAW DWG 657N4311, REV, AND SRM 51-40-02-0G.
- [SDR FDEA201701110122](https://openairdocs.org/sdr/FDEA201701110122.md): Cover · loose · Jan 11, 2017 · N928FD · Boeing 75728A · Escape Slide
  > CAN NOT ARM LEFT MAIN ENTRY DOOR SLIDE. FOUND LOWER SLIDE COVER LOOSE, REMOVED SLIDE COVER AND FOUND THE HOOK AND LOOP STRAPS LOOSE THAT STOW THE MATERAL TO THE GIRT BAR. TIGHTENED THE HOOK AND LOOP STRAPS AND CLEANED THE GIRT BAR MECHANISM AND SENSORS ON
- [SDR FDEA201612064328](https://openairdocs.org/sdr/FDEA201612064328.md): Control Cable · out of adjust · Dec 6, 2016 · N928FD · Boeing 75728A · Landing Gear Steering System
  > ON EXITING RUNWAY TILLER STUCK HARD AT 45' POSITION DURING 90' LT TURN. UPON GETTING BACK ON CENTER LINE, TILLER REQUIRED.5 TO 1 INSIDE RT TO REMAIN IN POSITSION. IF RELEASED, ACFT TURNED HARD LT. ACFT TURNED HARD LT OF TAXIWAY. PROBLEM DID NOT OCCUR ON TAX
- [SDR FDEA201607212593](https://openairdocs.org/sdr/FDEA201607212593.md): Hydraulic Line · leaking · Jul 21, 2016 · N928FD · Boeing 75728A · Hydraulic System, Main
  > DURING CLIMBOUT, RECEIVED LT HYD SYS LOW QUANTITY MESSAGE. SHORTLY, RECEIVED LT HYD SYS PRESSURE MESSAGE. COMPLIED WITH QRH EXTEND FLAPS ALTERNATELY AND ALTERNATELY EXTEND LANDING GEAR. FOUND LEFT MAIN GEAR DOWN LOCK ACTUATOR PRESSURE LINE LEAKING. REPLA
- [SDR FDEA201412194152](https://openairdocs.org/sdr/FDEA201412194152.md): Line · out of position · Dec 19, 2014 · N928FD · Boeing 75728A · Crew Oxygen System
  > LEFT COURIER SEAT O2 MASK DOES NOT TEST. AMM SMP UPON INSPECTION OF NR 1 COURIER MASK, FOUND OXYGEN LINES IMPROPERLY STOWED. STOWED MASK & LINES IAW AMM 35-11-00-2-99. SYS OPERATES NORMALLY IAW AMM 35-11-00-5. NO LEAKS OR DEFECTS NOTED AT THIS TIME.
- [SDR FDEA201410223331](https://openairdocs.org/sdr/FDEA201410223331.md): Panel · not seated · Oct 22, 2014 · N928FD · Boeing 75728A · Passenger/Crew Doors
  > L1 DOOR SLIDE WOULD NOT ARM PROPERLY BEFORE PUSHBACK. THE POP OUT ARMED PANEL STAYS FLUSH AGAINST THE DOOR WHEN THE EVACUATION SLIDE LEVER IS MOVED TO THE ARMED POSITION. FOUND CTR PANEL OUT OF TRACK, RESEATED CTR DOOR PANEL. GND TESTED NORMAL IAW SMP.
- [SDR FDEA201410213327](https://openairdocs.org/sdr/FDEA201410213327.md): Bracket · broken · Oct 21, 2014 · N928FD · Boeing 75728A · Escape Slide
  > SLIDE COVER LOOSE & NOT ATTACHED PROPERLY AT THE BOTTOM OF THE L1 DOOR. FOUND TOP LT BRACKET BROKEN ON SLIDE RAFT COVER. INSTALLED SERVICEABLE SLIDE COVER
- [SDR FDEA201406071327](https://openairdocs.org/sdr/FDEA201406071327.md): Bolt · sheared · Jun 7, 2014 · N928FD · Boeing 75728A · Rudder Control System
  > DURING TAXI OUT, CAPTAIN'S RT RUDDER PEDAL BROKE AS THE PARKING BRAKE WAS BEING SET. RT PEDAL MOVES FREELY WITH NO EFFECT ON FLIGHT CONTROLS. FOUND THE BOLT WHERE THE RT RUDDER PEDAL PUSHROD ATTACHES TO THE RUDDER PEDAL ARM TO BE SHEARED. REF IPC 24-21-02-
- [SDR FDEA201307091510](https://openairdocs.org/sdr/FDEA201307091510.md): Cover · loose · Jul 9, 2013 · N928FD · Boeing 75728A · Escape Slide
  > LEFT ENTRY DOOR SLIDE COVER IS LOOSE. TIGHTENED LOWER STRAP. OPS CHECKED NORMAL.
- [SDR FDEA201303170589](https://openairdocs.org/sdr/FDEA201303170589.md): Shear Tie · cracked · Mar 17, 2013 · N928FD · Boeing 75728A · Fuselage Internal Mounting Structure
  > AFT CARGO BS 1300 FRAME HAS A CRACKED SHEAR TIE BETWEEN S20-21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW DRAWING 140N2002 AND SRM 51-40-02
- [SDR FDEA201303120553](https://openairdocs.org/sdr/FDEA201303120553.md): Skin · dented · Mar 12, 2013 · N928FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED LEFT SIDE BS 637, STR 20L. CUT OUT DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-01 REPAIR 15 AND SRM 53-00-00.
- [SDR FDEA201208112954](https://openairdocs.org/sdr/FDEA201208112954.md): Cover · loose · Aug 11, 2012 · N928FD · Boeing 75728A · Escape Slide
  > L-1 DOOR SLIDE HOUSING IS LOOSE. RETIGHTENED SLIDE COVER IAW 25-66-01-414-101, FIG 402. OK FOR SERVICE.
- [SDR FDEA201204031237](https://openairdocs.org/sdr/FDEA201204031237.md): Bracket · backed out · Apr 3, 2012 · N928FD · Boeing 75728A · Passenger/Crew Doors
  > L1 ENTRY DOOR IS VERY DIFFICULT TO CLOSE. LOWER RT SIDE OF DOOR IS NOT ALIGNING PROPERLY AND IT TAKES SEVERAL ATTEMPTS TO CLOSE. REF PRIOR WRITE UPS. QTY 2 FITTING MSN 1267859 DURING GVI FWD UPPER AND LOWER FITTINGS IN DOOR FRAME HAVE LIGHT GOUGES FROM ROL
- [SDR FDEA201109213997](https://openairdocs.org/sdr/FDEA201109213997.md): Acm · failed · Sep 21, 2011 · N928FD · Boeing 75728A · Cabin Cooling System
  > AFTER ENGINES STARTED, AN ACRID ODOR SEEMED TO ORIGINATE FROM THE LT PACK. WE ALSO HEARD A WHINNING NOISE AS THE THRUST LEVERS WERE ADVANCED. BOTH THE SMELL AND THE WHINE DID NOT RECUR WITH THE LT PACK OFF. INWORK. TROUBLESHOT AND FOUND ACM NOT TURNING WH
- [SDR FDEA201108203390](https://openairdocs.org/sdr/FDEA201108203390.md): Sensor · out of adjust · Aug 20, 2011 · N928FD · Boeing 75728A · Door Warning System
  > EICAS RT EMERGENCY DOOR AND OVERHEAD EMERGENCY DOOR LIGHT ON MOST OF FLIGHT. OFF DURING DESCENT. ADJUSTED DOOR PROX SENSOR GAP. OPS CHECKS GOOD.
- [SDR FDEA201108053104](https://openairdocs.org/sdr/FDEA201108053104.md): Duct · disconnected · Aug 5, 2011 · N928FD · Boeing 75728A · Air Distribution System
  > ON DEPARTURE WITH LT PACK MEL'D, RECEIVED "RT PACK TRIP". COULD NOT PRESSURIZE ACFT. FOUND DUCT DISCONNECTED FROM TOP OF R/H HEAT EXCHANGER AND FROM THE ACM COMPRESSOR OUTLET, INSTALLED DUCT WITH NEW COUPLER AND PERI SEALS IAW AMM ACM. R & R SECTION. FOUND

Next page: https://openairdocs.org/aircraft/N928FD/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N928FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N928FD/reports

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